CN206278281U - Two axle gondolas and unmanned vehicle - Google Patents
Two axle gondolas and unmanned vehicle Download PDFInfo
- Publication number
- CN206278281U CN206278281U CN201621188835.5U CN201621188835U CN206278281U CN 206278281 U CN206278281 U CN 206278281U CN 201621188835 U CN201621188835 U CN 201621188835U CN 206278281 U CN206278281 U CN 206278281U
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- Prior art keywords
- rotary body
- gondola
- connecting portion
- actuator
- inner housing
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Abstract
The utility model belongs to unmanned air vehicle technique field, discloses a kind of two axles gondola and unmanned vehicle, including：Quick Release connector pair, the secondary first connecting portion of the Quick Release connector is used to connect the fuselage of unmanned vehicle, and the secondary second connecting portion of the Quick Release connector is locked in the first connecting portion；First rotary body, is rotatably fixed in the second connecting portion, can rotate in the horizontal plane；Second rotary body, is embedded in first a rotating body, is pivotally connected with first rotary body, can be in vertical rotation in surface；Camera head, is fixed on second a rotating body, follows second rotary body to move, shooting angle in adjustment vertical plane；First rotary body is followed to move, the shooting angle in adjustment horizontal plane；Gondola controls circuit, is connected with first rotary body, the second rotary body and the camera head respectively.The utility model provides a kind of simple structure, lightweight, and the unmanned vehicle of simple operation is with two axle gondolas.
Description
Technical field
The utility model is related to unmanned air vehicle technique field, more particularly to a kind of two axles gondola and unmanned vehicle.
Background technology
Unmanned vehicle in flight course, because job requirements generally require to adopt the relevant information in way in real time
Collection, image such as on the way, video information.Thus, it is of the prior art that capture apparatus are carried using unmanned flight's equipment more
Mode, random shooting.
But with the variation of purposes, often structure is answered to cause airborne equipment and the fixed connection structure that is attached thereto
Miscellaneous, operation inconvenience, while the weight for being also is very big, has a strong impact on flight efficiency, safety and shooting operation.
Utility model content
The utility model provides a kind of two axles gondola, solves unmanned flight's equipment carrying structure complexity in the prior art, behaviour
Make inconvenience, the big technical problem of weight.
In order to solve the above technical problems, the utility model provides a kind of two axles gondola, for unmanned vehicle；Including：
Quick Release connector pair, the secondary first connecting portion of the Quick Release connector is used to connect the fuselage of unmanned vehicle,
The secondary second connecting portion of the Quick Release connector is locked in the first connecting portion；
First rotary body, first rotary body is rotatably fixed in the second connecting portion, can be turned in the horizontal plane
It is dynamic；
Second rotary body, second rotary body is embedded in first a rotating body, is pivoted with first rotary body and connected
Connect, can be in vertical rotation in surface；
Camera head, the camera head is fixed on second a rotating body, follows second rotary body to move, and adjusts
Shooting angle in whole vertical plane；First rotary body is followed to move, the shooting angle in adjustment horizontal plane；
Gondola controls circuit, is connected with first rotary body, the second rotary body and the camera head respectively.
Further, first rotary body includes：
Shell body, the shell body is rotatably fixed in the second connecting portion；Second rotary body is fixed on institute
State on shell body；
First actuator, first actuator is connected between the second connecting portion and the shell body, for driving
The shell body is rotated, and is connected with gondola control circuit.
Further, the shell body is in hollow ball-shape structure；Including：
The first actuator connecting portion at the top of the chondritic, for being fixedly connected first actuator；Institute
The first actuator connecting portion is stated to be rotatably fixed in the second connecting portion；
Positioned at the pivotal support arm that the side of the chondritic is oppositely arranged, for connecting support second rotation
Body；
Wherein, second rotary body is pivotally connected with the pivotal support arm, for being rotated relative to the shell body,
To adjust the shooting angle in perpendicular.
Further, second rotary body includes：
Inner housing, the inner housing is rotatably fixed on the pivotal support arm, can be rotated relative to the shell body；
Second actuator, second actuator is connected between the pivotal support arm and the shell body, for driving
The inner housing is rotated, and is connected with gondola control circuit.
Further, the inner housing is in hollow ball-shape structure；
The camera head is fixed in the inner housing；
The inner housing side, sets the second actuator connecting portion, for fixing with the rotation supporting cantilever junction
Connect second actuator；
The inner housing opposite side, sets with the rotation supporting cantilever junction and is flexibly connected with the pivotal support arm
Rotating shaft, be embedded in it is described rotation supporting cantilever in.
Further, second rotary body also includes：Radiator fan；
The radiator fan is fixed in the inner housing；
Louvre is opened up on the inner housing.
Further, the inner housing includes：Protecgulum and matching bonnet；
Device window, the fixation camera head lens are opened up on the protecgulum；
HDMI is set on the inner housing, is connected with the camera head.
Further, the gondola control circuit includes：Control circuit and fixed structure；
The control circuit is fixed in the fixed structure, respectively with first actuator, second actuator
And the camera head is connected；
The fixed structure is arranged between the second connecting portion and the shell body, the shell body rotationally with
The fixed structure is connected.
Further, it is dovetail groove connector pair that the Quick Release connector is secondary.
A kind of unmanned vehicle, including：Two axle gondolas described in fuselage and any of the above-described；
The two axles gondola is connected to the fuselage bottom；
The gondola control circuit connects the flight controller of the fuselage.
One or more technical schemes provided in the embodiment of the present application, at least have the following technical effect that or advantage：
The unmanned vehicle provided in the embodiment of the present application, by optimizing the rotational structure and connected mode of gondola, simplifies
Carrying structure；Specifically, by separate horizontal rotary body and vertical rotor, realize that the shooting angle of two dimension is adjusted
Whole structure, simplifies rotary control structure, so that while loss of weight so that shoot control operation smooth；Meanwhile, connected using Quick Release
Connected components are connected with fuselage, so that the dismounting that carrying equipment can be rapidly and efficiently so that the more convenient side of the maintenance of gondola
Just.
Further, used by the way that the shell body of hollow ball-shape is mutually nested with inner housing, coordinated using spherical track
Attribute so that the main structure body of gondola significantly simplifies, and further mitigates weight.
Brief description of the drawings
The front view of the two axle gondolas that Fig. 1 is provided for the utility model；
Fig. 2 is the side view of Fig. 1；
Fig. 3 is the explosive view of Fig. 1.
Specific embodiment
The embodiment of the present application solves unmanned flight's equipment carrying structure in the prior art and answers by providing a kind of two axles gondola
It is miscellaneous, operation inconvenience, the big technical problem of weight；Simplified carrying structure, lifting operation fluency and efficiency have been reached, weight has been reduced
Technique effect.
In order to solve the above technical problems, the general thought that the embodiment of the present application provides technical scheme is as follows：
By optimizing the rotational structure and connected mode of gondola, carrying structure is simplified；Specifically, by separate
Horizontal rotary body and vertical rotor, realize two dimension shooting angle adjustment structure, rotary control structure is simplified, so as to subtract
While weight so that shoot control operation smooth；Meanwhile, it is connected with fuselage using Quick Release coupling assembly, so that carrying sets
Standby dismounting that can be rapidly and efficiently so that the more convenient convenience of the maintenance of gondola.
Below in conjunction with the accompanying drawing in the utility model embodiment, the technical scheme in the utility model embodiment is carried out
Clearly and completely describe, it is clear that described embodiment is only a part of embodiment of the utility model, rather than whole
Embodiment.Based on the embodiment in the utility model, the every other embodiment that those of ordinary skill in the art are obtained all belongs to
In the scope of the utility model protection；"and/or" keyword wherein involved in this implementation, represent and or two kinds of situations, change
Sentence is talked about, and A and/or B mentioned by the utility model embodiment illustrate A and B, two kinds of situations of A or B, describe A and B and are deposited
Three kinds of states, such as A and/or B, represent：Only including A does not include B；Only including B does not include A；Including A and B.
Meanwhile, in the utility model embodiment, when component is referred to as " being fixed on " another component, it can be directly another
On one component or can also there is component placed in the middle.When a component is considered as " connection " another component, it can be
It is directly connected to another component or may be simultaneously present component placed in the middle.When component be considered as " being arranged at " another
Component, it can be set directly on another component or may be simultaneously present component placed in the middle.The utility model embodiment
Used in term " vertical ", " level ", "left", "right" and similar statement be merely for purposes of illustration, not
It is intended to limit the utility model.
Referring to Fig. 1~3, the present embodiment provides a kind of two axle gondolas for being applied to unmanned vehicle；The two axles gondola bag
Include：Gondola control circuit, Quick Release connector pair, the first rotary body, the second rotary body and camera head 19.
The secondary first connecting portion of the Quick Release connector is used to connect the fuselage of unmanned vehicle, the Quick Release connector
Secondary second connecting portion 1 is locked in the first connecting portion；Form the attachment structure of gondola and upper unmanned vehicle.
First rotary body is rotatably fixed in the second connecting portion 1, can be rotated in the horizontal plane；I.e. relative to
Upper unmanned flight's equipment, rotates in the horizontal plane.
Second rotary body is embedded in first a rotating body, is pivotally connected with first rotary body, can be vertical
Rotation in surface；I.e. relative to the first rotary body and upper unmanned flight's equipment, rotate in the horizontal plane.
The camera head is fixed on second a rotating body, follows second rotary body to move, and adjusts vertical plane
Interior shooting angle；First rotary body is followed to move, the shooting angle in adjustment horizontal plane.
Gondola controls circuit, is connected with first rotary body, the second rotary body and the camera head respectively.Realize
Rotate and shoot control.
For first rotary body, including：The actuator 11 of shell body 20 and first.
The shell body 20 is rotatably fixed in the second connecting portion 1；Second rotary body is fixed on described outer
On housing 20；Can be rotated relative to protected shell body 20, so as to realize angle again on the basis of the rotation of the first rotary body
Adjustment.
First actuator 11 is connected between the second connecting portion 1 and the shell body 20, described outer for driving
Housing 20 is rotated；In the control line action of gondola control circuit.
For shell body 20, the shell body 20 is in hollow ball-shape structure；Including：At the top of the chondritic
First actuator connecting portion and the pivotal support arm being oppositely arranged positioned at the side of the chondritic.I.e. on hemispherical top
Portion forms the first actuator connecting portion, and two pivotal support arms are set in bottom symmetrical position.
First actuator connecting portion, for being fixedly connected first actuator；The first actuator connecting portion is rotated
Be fixed in the second connecting portion 1；The fixing end and turning end of i.e. described first actuator connect described first and drive respectively
Moving part connecting portion and the second connecting portion 1, constitute the driven rotational structure of stabilization.
The pivotal support arm being oppositely arranged, for connecting support second rotary body；Second rotary body with it is described
Pivotal support arm is pivotally connected, for being rotated relative to the shell body, to adjust the shooting angle in perpendicular.That is, exist
Complete to realize numerical value angle adjustment while level angle is adjusted.
For second rotary body, second rotary body includes：Between inner housing (13 and 14) and the second driving
18。
The inner housing is rotatably fixed between the pivotal support arm, can be rotated relative to the shell body 20；It is described
Second actuator 18 is connected between the pivotal support arm and the shell body, for driving the inner housing to rotate；By described
Gondola control circuit control.
For the inner housing, the inner housing is in hollow ball-shape structure；The camera head 19 is fixed in described
In housing, movement is followed.
The inner housing side, sets the second actuator connecting portion, for fixing with the rotation supporting cantilever junction
Connect second actuator；What is matched sets the second actuator draw-in groove herein in supporting cantilever, driven with described second
Part connecting portion connect respectively it is described second drive between 18 fixing end and turning end.Form the driven rotational structure of stabilization.
The inner housing opposite side, sets with the rotation supporting cantilever junction and is flexibly connected with the pivotal support arm
Rotating shaft 16, be embedded in it is described rotation supporting cantilever in.And fixed by locking member 15.
Further, second rotary body also includes：Radiator fan 17；The radiator fan 17 is fixed on the inner casing
In vivo；Match, louvre is opened up on the inner housing.
For the inner housing, the inner housing includes：Protecgulum 14 and matching bonnet 13.
Device window, the camera lens of the fixation camera head 19 are opened up on the protecgulum 14；Set on the inner housing
HDMI, is connected with the camera head 19, is easy to obtain photographed data, it is to avoid dismounting gondola.
For gondola control circuit, the gondola control circuit includes：Control circuit and fixed structure.
The control circuit is fixed in the fixed structure, is driven with first actuator 11, described second respectively
Part 18 and the camera head 19 are connected；Set up control structure.
The fixed structure is arranged between the second connecting portion 1 and the shell body 20,20 turns of the shell body
Dynamic ground is connected with the fixed structure.
The control circuit connection fuselage flight controller；For obtaining flight control command, the shooting angle of gondola is performed
Degree adjustment.
Be necessary explanation, control circuit directly control perform rotation process driver part, with realize horizontal plane and
Rotation control in vertical plane.
The control circuit can be divided into according to function：Equipment control circuit 5 and rotation control circuit 4, mu balanced circuit 6
It is respectively used to the capture apparatus that control is carried, such as camera head 19；And actuator.
For the fixed structure, including：Upper damping carbon plate 10 and lower damping carbon plate 12；First actuator 11 is consolidated
It is scheduled between the upper damping carbon plate 10 and lower damping carbon plate 12, and is fixedly linked with the upper damping carbon plate 10, suppresses first
The vibration of actuator 11.
The fixed structure also includes：Fixed seat 7 and upper lid 3；The control circuit is fixed in the fixed seat 7,
And compressed by upper lid 3.The fixed seat 7 is fixed on the upper damping carbon plate 10.
Preferably, HIMI interfaces 9 are opened up in the fixed seat 7, even connection control circuit, obtains photographing information.
For Quick Release connector pair, including two locking members of mutual cooperation.Specifically, the Quick Release connector
Secondary first connecting portion is fixed on the fuselage, static with respect to fuselage, the secondary second connecting portion locking of the Quick Release connector
In the first connecting portion；Now, the second connecting portion is also static with respect to fuselage.
Specifically, it is dovetail groove connector pair that the Quick Release connector is secondary；Put down on dovetail groove and be fixed on fuselage, dovetail
1 is put down under groove to be fixed on the fixed structure.
Specifically, 1 time is put down under the dovetail groove and passes through dovetail groove connecting plate 2 and connecting pole 8 and the lower damping
Carbon plate 12 is fixedly linked, so as to quick-disassembly structure be connected with the first rotary body.
The present embodiment also provides a kind of unmanned vehicle based on above-mentioned two axles gondola.
A kind of unmanned vehicle, including：Fuselage and above-mentioned two axles gondola；
The two axles gondola is connected to the fuselage bottom；
The gondola control circuit connects the flight controller of the fuselage.
One or more technical schemes provided in the embodiment of the present application, at least have the following technical effect that or advantage：
The unmanned vehicle provided in the embodiment of the present application, by optimizing the rotational structure and connected mode of gondola, simplifies
Carrying structure；Specifically, by separate horizontal rotary body and vertical rotor, realize that the shooting angle of two dimension is adjusted
Whole structure, simplifies rotary control structure, so that while loss of weight so that shoot control operation smooth；Meanwhile, connected using Quick Release
Connected components are connected with fuselage, so that the dismounting that carrying equipment can be rapidly and efficiently so that the more convenient side of the maintenance of gondola
Just.
Further, used by the way that the shell body of hollow ball-shape is mutually nested with inner housing, coordinated using spherical track
Attribute so that the main structure body of gondola significantly simplifies, and further mitigates weight.
It should be noted last that, above specific embodiment is only used to illustrate the technical solution of the utility model rather than limit
System, although being described in detail to the utility model with reference to example, it will be understood by those within the art that, can be right
The technical solution of the utility model is modified or equivalent, without deviating from the spirit and model of technical solutions of the utility model
Enclose, it all should cover in the middle of right of the present utility model.
Claims (10)
1. a kind of two axles gondola, for unmanned vehicle；It is characterised in that it includes：
Quick Release connector pair, the secondary first connecting portion of the Quick Release connector is used to connect the fuselage of unmanned vehicle, described
The secondary second connecting portion of Quick Release connector is locked in the first connecting portion；
First rotary body, first rotary body is rotatably fixed in the second connecting portion, can be rotated in the horizontal plane；
Second rotary body, second rotary body is embedded in first a rotating body, is pivotally connected with first rotary body, can
In vertical rotation in surface；
Camera head, the camera head is fixed on second a rotating body, follows second rotary body to move, and adjustment is perpendicular
Face interior shooting angle directly；First rotary body is followed to move, the shooting angle in adjustment horizontal plane；
Gondola controls circuit, is connected with first rotary body, the second rotary body and the camera head respectively.
2. two axles gondola as claimed in claim 1, it is characterised in that first rotary body includes：
Shell body, the shell body is rotatably fixed in the second connecting portion；Second rotary body is rotatably fixed to
On the shell body；
First actuator, first actuator is connected between the second connecting portion and the shell body, described for driving
Shell body is rotated, and is connected with gondola control circuit.
3. two axles gondola as claimed in claim 2, it is characterised in that：The shell body is in hollow ball-shape structure；Including：
The first actuator connecting portion at the top of the chondritic, for being fixedly connected first actuator；Described
One actuator connecting portion is rotatably fixed in the second connecting portion；
Positioned at the pivotal support arm that the side of the chondritic is oppositely arranged, for connecting support second rotary body；
Wherein, second rotary body is pivotally connected with the pivotal support arm, for being rotated relative to the shell body, to adjust
Shooting angle in whole perpendicular.
4. two axles gondola as claimed in claim 3, it is characterised in that second rotary body includes：
Inner housing, the inner housing is rotatably fixed on the pivotal support arm, can be rotated relative to the shell body；
Second actuator, second actuator is connected between the pivotal support arm and the shell body, described for driving
Inner housing is rotated, and is connected with gondola control circuit.
5. two axles gondola as claimed in claim 4, it is characterised in that：The inner housing is in hollow ball-shape structure；
The camera head is fixed in the inner housing；
The inner housing side, sets the second actuator connecting portion, for being fixedly connected with the rotation supporting cantilever junction
Second actuator；
The inner housing opposite side, with turning that rotation supporting cantilever junction setting is flexibly connected with the pivotal support arm
Axle, is embedded in the rotation supporting cantilever.
6. two axles gondola as claimed in claim 5, it is characterised in that second rotary body also includes：Radiator fan；
The radiator fan is fixed in the inner housing；
Louvre is opened up on the inner housing.
7. two axles gondola as claimed in claim 6, it is characterised in that the inner housing includes：Protecgulum and matching
Bonnet；
Device window, the fixation camera head lens are opened up on the protecgulum；
HDMI is set on the inner housing, is connected with the camera head.
8. two axle gondolas as described in any one of claim 4~7, it is characterised in that the gondola control circuit includes：Control
Circuit and fixed structure；
It is described control circuit be fixed in the fixed structure, respectively with first actuator, second actuator and
The camera head is connected；
The fixed structure is arranged between the second connecting portion and the shell body, the shell body rotationally with it is described
Fixed structure is connected.
9. two axles gondola as claimed in claim 8, it is characterised in that：It is dovetail groove connector pair that the Quick Release connector is secondary.
10. a kind of unmanned vehicle, it is characterised in that including：Fuselage and two axles as described in any one of claim 1~9
Gondola；
The two axles gondola is connected to the fuselage bottom；
The gondola control circuit connects the flight controller of the fuselage.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621188835.5U CN206278281U (en) | 2016-10-28 | 2016-10-28 | Two axle gondolas and unmanned vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621188835.5U CN206278281U (en) | 2016-10-28 | 2016-10-28 | Two axle gondolas and unmanned vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206278281U true CN206278281U (en) | 2017-06-27 |
Family
ID=59082326
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621188835.5U Expired - Fee Related CN206278281U (en) | 2016-10-28 | 2016-10-28 | Two axle gondolas and unmanned vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206278281U (en) |
-
2016
- 2016-10-28 CN CN201621188835.5U patent/CN206278281U/en not_active Expired - Fee Related
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20170627 Termination date: 20181028 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |